EP0472566A1 - Übertragungsvorrichtung am flugzeug beim aufnehmen der bugräder - Google Patents

Übertragungsvorrichtung am flugzeug beim aufnehmen der bugräder

Info

Publication number
EP0472566A1
EP0472566A1 EP90907075A EP90907075A EP0472566A1 EP 0472566 A1 EP0472566 A1 EP 0472566A1 EP 90907075 A EP90907075 A EP 90907075A EP 90907075 A EP90907075 A EP 90907075A EP 0472566 A1 EP0472566 A1 EP 0472566A1
Authority
EP
European Patent Office
Prior art keywords
wheels
friction rollers
transfer device
bogie
rollers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP90907075A
Other languages
English (en)
French (fr)
Inventor
Matti Sinkkonen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tana-Jyra Ky
Original Assignee
Tana-Jyra Ky
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tana-Jyra Ky filed Critical Tana-Jyra Ky
Publication of EP0472566A1 publication Critical patent/EP0472566A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/22Ground or aircraft-carrier-deck installations for handling aircraft
    • B64F1/223Ground or aircraft-carrier-deck installations for handling aircraft for towing aircraft
    • B64F1/225Vehicles specially adapted therefor, e.g. aircraft tow tractors
    • B64F1/227Vehicles specially adapted therefor, e.g. aircraft tow tractors for direct connection to aircraft, e.g. tow tractors without towing bars

Definitions

  • the object of the invention is a transfer device that grips bogies, which is intended to move an aircraft or other device equipped with bogie wheels over a base, which transfer device includes a frame component and supported on this friction rollers that grip four or two in-line bogie wheels and rotate them, and motors to drive the rollers, at least three rollers per wheel, and pressure devices to press the friction rollers against the wheels, and which transfer device includes a power source and transmission equipment to feed the driving power to the motors and devices to place the friction rollers around the wheels and to remove them from the wheels.
  • the construction of a transfer device can be substantially lightened if the rotational force is transferred to the air ⁇ craft's own wheel from a drive wheel or friction roller belon ⁇ ging to the transfer device.
  • a construction for a completely general purpose transfer device is shown is Finnish Patent Application FI 833275 (partly corresponding to 085/ 01265) . This requires no contact with the bogie of the aircraft to press the drive wheel against the aircraft wheel. The pressure is created by means of the mutual movement of pressure rollers placed around the wheel of the aircraft and connected by an intermediate member.
  • the intermediate member draws the two pressure rollers connected by it towards one another, when they are pressed against the wheel between them. At least one of the pressing wheels is now a friction roller or drive wheel, which transmits rotational force to the wheel of the aircraft.
  • Other transfer devices belonging to the field of the invention are shown in Finnish Patent Applications FI861714, FI870313, and FI870710 and in USA Patent US 3,005,510. In practice nearly all aircraft are equipped with either double wheels or still larger bogie wheels.
  • a transfer device that grips bogie wheels is shown in the aforementioned PCT publication O85/01265. This is shown in Figures 10-13, 15, 19, 20, and 22-23 of this publication. In all the forms of application referred to two in-line wheels are together pressed by rotating friction rollers. This stresses the bogie considerably nor is this generally permitted by aircraft manufacturers. This is because bogies are in no way dimensioned to withstand a load pressing the axles together. Only in connec ⁇ tion with the final form of application, in Figures 19, 20, and 22-23, is one method of placing the friction rollers around the wheel shown. Bringing the transfer device straight from the side means that friction rollers can only be located on one side of this unit, which is highly impractical.
  • a transfer device that grips the nose bogie wheels is shown in US Patent Publication 3,005,510.
  • the bogie wheels next to each other are driven by means of two friction roller mats, which are wedged between the in-line bogie wheels.
  • a force is caused between the axles, which tends to force the axles apart.
  • This invention presents a new type of bogie-gripping transfer device.
  • the practical problems connected to a bogie-gripping transfer device are, among others:
  • the intention of this invention is to create a transfer device rotating different kinds of bogie wheels, in which the afore ⁇ mentioned problems have been overcome.
  • the characteristics of the invention appear in the accompanying Patent Claim 1.
  • the main principle of the invention is to form a floating support for the friction rollers gripping the wheels of the second axle of the bogie. These are permitted a unified movement is location in a horizontal direction, by means of which they can be applied to an arbitrary distance between axles.
  • the symmetrical location of the friction rollers achieves the advantage that the greatest part of the compressive force caused by the torque is cancelled out.
  • symmetrical pairs of friction rollers are self- centering, when they are drawn towards one another.
  • the form of application in accordance with Patent Claim 3 solves in a simple manner the pre-setting of the transfer device to sets of bogie wheels of different size. According to this the rear friction rollers can be driven up to the bogie wheels, when a clear fixed point for placing is created. This can be achieved even more advantageously in accordance with Patent Claim 5, when the same transfer device can be applied to dealing with a large range of differently sized bogie wheels. Placing takes place quickly, when the rear friction rollers are placed beforehand in a setting corresponding to the size of the bogie wheel.
  • the form of application in accordance with Patent Claim 4 shows placing members for a transfer device, which only take up a small space longitudinally.
  • Figures l and 2 show the use of the transfer device in moving an aircraft
  • Figure 3 shows the transfer device being driven round a set of bogie wheels
  • Figure 4 shows the transfer device seen from in front
  • Figure 5 shows the transfer device in the transfer position, attached to the bogie
  • Figure 6 shows the situation in Figure 5 seen from above
  • Figure 7 shows a cross-section of Figure 5 at I - I.
  • the transfer device 2 pushes the aircraft 1 from the right-hand side, fixed under ⁇ carriage bogie in which there is the set of bogies wheels 3.
  • the pushing causes a turning moment around the left-hand side undercarriage, which is cancelled out by the lateral frictional force nosewheel 5 of the aircraft and the main undercarriage beneath the fuselage.
  • the aircraft 1 is pushed back ⁇ wards, when the transfer device 2 is brought around the set of bogie wheels from in front. It is also possible to push the aircraft 1 using the transfer device 2.
  • the transfer device 2 is being driven around the set of bogie wheels. The driver is not shown. Before attachment to the bogie wheels the steering of the transfer device 2 takes place by means of the steerable rear wheel 7. The other wheels 5 of the control cab frame 4 are then locked. Hydraulic motors are attached to these wheels for the independent movement of the transfer device 2.
  • the transfer device 2 is composed of two main parts; the control cab frame 4 and the pairs of friction rollers and placing devices carried by the frame component 8, 18.
  • the control cab frame 4 contains power and control devices.
  • the power devices consist of a diesel motor and a hydraulic pump unit.
  • a chain is arranged to run round the length of slide 12, the motor unit being attached to the chain.
  • the chain is driven by a chain mechanism, which is driven from the longi ⁇ tudinal axle 26. This has a wedge groove formed in its entire length, by means of which the torque can be transmitted to the chain mechanism 25 as it moves with slide 10 or 11.
  • the axle 26 is connected to the drive shaft from the gearbox of the drive motor 27 and drives all three slides 12 in the same row.
  • the various dimensions of the set of bogie wheels 3 of the aircraft to be moved are generally known and in accordance with this the rear friction rollers 15 can be set to such a position before moving that the central slides 10 come exactly between the bogie wheels 6.
  • the pre-setting of the slide 9 takes place by means of cylinder 24, which also locks to the desired place.
  • the middle and front friction rollers 14 are pushed in at the location of the wheels 6.
  • Cylinders 23 and 24 are pushed completely out, when they push slides 10 and 11 to their extreme positions against stops 21 and 22.
  • the frame 8 is still carried on wheels 17 and the lower end of the vertical slide 19 and the upper 14 and 15 are only slightly above the centre line of the wheel 6.
  • the pressure of the friction wheels 14 and 15 against the wheel 6 is created by drawing the front slides 10 and 15 together by means of cylinder 20 and the second last slide 10 backwards by means of cylinder 23.
  • the outputs of cylinders 20 and 23 are arranged to be equally great, in which case the same static pressure is applied to all friction wheels 14 and 15.
  • Each friction roller must be pressed against wheel 6 with such a great force, that the necessary transfer of the friction force to wheel 6 is in general possible.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Handcart (AREA)
  • Arrangement And Driving Of Transmission Devices (AREA)
EP90907075A 1989-05-18 1990-05-17 Übertragungsvorrichtung am flugzeug beim aufnehmen der bugräder Withdrawn EP0472566A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FI892379A FI81536C (fi) 1989-05-18 1989-05-18 Vid boggihjul gripande foerflyttningsanordning.

Publications (1)

Publication Number Publication Date
EP0472566A1 true EP0472566A1 (de) 1992-03-04

Family

ID=8528451

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90907075A Withdrawn EP0472566A1 (de) 1989-05-18 1990-05-17 Übertragungsvorrichtung am flugzeug beim aufnehmen der bugräder

Country Status (3)

Country Link
EP (1) EP0472566A1 (de)
FI (1) FI81536C (de)
WO (1) WO1990014268A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006053476A1 (fr) * 2004-11-22 2006-05-26 Min Cai Dispositif automatique de fixation de vehicules

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
HU193236B (en) * 1983-09-13 1987-08-28 Matti Sinkkonen Mechanism for moving wheeled vehicles by friction auxiliary drive

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9014268A1 *

Also Published As

Publication number Publication date
FI81536C (fi) 1990-11-12
WO1990014268A1 (en) 1990-11-29
FI892379A0 (fi) 1989-05-18
FI81536B (fi) 1990-07-31

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Legal Events

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Effective date: 19921201